ATE298460T1 - HALL EFFECT PLASMA ACCELERATOR - Google Patents
HALL EFFECT PLASMA ACCELERATORInfo
- Publication number
- ATE298460T1 ATE298460T1 AT96308748T AT96308748T ATE298460T1 AT E298460 T1 ATE298460 T1 AT E298460T1 AT 96308748 T AT96308748 T AT 96308748T AT 96308748 T AT96308748 T AT 96308748T AT E298460 T1 ATE298460 T1 AT E298460T1
- Authority
- AT
- Austria
- Prior art keywords
- magnetic field
- hall effect
- channel
- source
- plasma accelerator
- Prior art date
Links
- 230000005355 Hall effect Effects 0.000 title abstract 3
- 230000001133 acceleration Effects 0.000 abstract 1
- 238000010438 heat treatment Methods 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H1/00—Using plasma to produce a reactive propulsive thrust
- F03H1/0037—Electrostatic ion thrusters
- F03H1/0062—Electrostatic ion thrusters grid-less with an applied magnetic field
- F03H1/0075—Electrostatic ion thrusters grid-less with an applied magnetic field with an annular channel; Hall-effect thrusters with closed electron drift
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/405—Ion or plasma engines
Abstract
A Hall effect plasma accelerator comprises an annular accelerating channel having closed and open ends. A source of magnetic field is positioned behind the closed end of the channel and has an axis extending in the same direction as the axis of the channel. This makes it possible to provide a Hall effect accelerator with an optimum distribution of magnetic field inside the acceleration channel by means of a simpler and less heavy arrangement using a single source of magnetic field, such as a single coil or permanent magnet. In addition it makes possible a reduction in heating of the source of magnetic field.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU9696105557A RU2092983C1 (en) | 1996-04-01 | 1996-04-01 | Plasma accelerator |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE298460T1 true ATE298460T1 (en) | 2005-07-15 |
Family
ID=20178385
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT96308748T ATE298460T1 (en) | 1996-04-01 | 1996-12-03 | HALL EFFECT PLASMA ACCELERATOR |
AT96308750T ATE298461T1 (en) | 1996-04-01 | 1996-12-03 | HALL EFFECT PLASMA ACCELERATOR |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT96308750T ATE298461T1 (en) | 1996-04-01 | 1996-12-03 | HALL EFFECT PLASMA ACCELERATOR |
Country Status (6)
Country | Link |
---|---|
US (2) | US5847493A (en) |
EP (2) | EP0800197B1 (en) |
AT (2) | ATE298460T1 (en) |
DE (2) | DE69634872T2 (en) |
RU (1) | RU2092983C1 (en) |
WO (1) | WO1997037519A1 (en) |
Families Citing this family (49)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5958157A (en) * | 1996-09-11 | 1999-09-28 | Sandia Corporation | Magnetic multipole redirector of moving plasmas |
US6215124B1 (en) | 1998-06-05 | 2001-04-10 | Primex Aerospace Company | Multistage ion accelerators with closed electron drift |
US6208080B1 (en) | 1998-06-05 | 2001-03-27 | Primex Aerospace Company | Magnetic flux shaping in ion accelerators with closed electron drift |
US6612105B1 (en) | 1998-06-05 | 2003-09-02 | Aerojet-General Corporation | Uniform gas distribution in ion accelerators with closed electron drift |
US6075321A (en) * | 1998-06-30 | 2000-06-13 | Busek, Co., Inc. | Hall field plasma accelerator with an inner and outer anode |
US6150764A (en) * | 1998-12-17 | 2000-11-21 | Busek Co., Inc. | Tandem hall field plasma accelerator |
FR2788084B1 (en) * | 1998-12-30 | 2001-04-06 | Snecma | PLASMA PROPELLER WITH CLOSED ELECTRON DRIFT WITH ORIENTABLE PUSH VECTOR |
US6787723B2 (en) * | 1999-03-24 | 2004-09-07 | The Regents Of The University Of Michigan | Method for laser induced isotope enrichment |
WO2000056428A2 (en) | 1999-03-24 | 2000-09-28 | The Regents Of The University Of Michigan | Method for laser induced isotope enrichment |
US6525480B1 (en) * | 1999-06-29 | 2003-02-25 | The Board Of Trustees Of The Leland Stanford Junior University | Low power, linear geometry hall plasma source with an open electron drift |
DE10014033C2 (en) * | 2000-03-22 | 2002-01-24 | Thomson Tubes Electroniques Gm | Plasma accelerator arrangement |
US6448721B2 (en) * | 2000-04-14 | 2002-09-10 | General Plasma Technologies Llc | Cylindrical geometry hall thruster |
US6777862B2 (en) * | 2000-04-14 | 2004-08-17 | General Plasma Technologies Llc | Segmented electrode hall thruster with reduced plume |
US6486593B1 (en) | 2000-09-29 | 2002-11-26 | The United States Of America As Represented By The United States Department Of Energy | Plasma accelerator |
DE10130464B4 (en) * | 2001-06-23 | 2010-09-16 | Thales Electron Devices Gmbh | Plasma accelerator configuration |
DE10153723A1 (en) * | 2001-10-31 | 2003-05-15 | Thales Electron Devices Gmbh | Plasma accelerator configuration |
FR2842261A1 (en) * | 2002-07-09 | 2004-01-16 | Centre Nat Etd Spatiales | HALL EFFECT PLASMIC PROPELLER |
US6696792B1 (en) | 2002-08-08 | 2004-02-24 | The United States Of America As Represented By The United States National Aeronautics And Space Administration | Compact plasma accelerator |
DE10300728B3 (en) * | 2003-01-11 | 2004-09-02 | Thales Electron Devices Gmbh | Ion accelerator arrangement |
DE10300776B3 (en) * | 2003-01-11 | 2004-09-02 | Thales Electron Devices Gmbh | Ion accelerator arrangement |
US7030576B2 (en) * | 2003-12-02 | 2006-04-18 | United Technologies Corporation | Multichannel hall effect thruster |
JP2006147449A (en) * | 2004-11-24 | 2006-06-08 | Japan Aerospace Exploration Agency | High-frequency discharge plasma generation type two-step hole effect plasma accelerator |
KR100599092B1 (en) | 2004-11-29 | 2006-07-12 | 삼성전자주식회사 | Electro-magnatic accelerator with driving frequency modulation |
KR100599094B1 (en) | 2004-11-29 | 2006-07-12 | 삼성전자주식회사 | Electro-magnatic accelerator with Coil turn modulation |
US7617092B2 (en) * | 2004-12-01 | 2009-11-10 | Microsoft Corporation | Safe, secure resource editing for application localization |
US7624566B1 (en) | 2005-01-18 | 2009-12-01 | The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration | Magnetic circuit for hall effect plasma accelerator |
US7500350B1 (en) | 2005-01-28 | 2009-03-10 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Elimination of lifetime limiting mechanism of hall thrusters |
US7679025B1 (en) * | 2005-02-04 | 2010-03-16 | Mahadevan Krishnan | Dense plasma focus apparatus |
KR100709354B1 (en) * | 2005-06-17 | 2007-04-20 | 삼성전자주식회사 | The multi-channel plasma accelerator |
KR100683174B1 (en) * | 2005-06-17 | 2007-02-15 | 삼성전자주식회사 | Plasma accelerating apparatus and plasma processing system having the same |
US8006939B2 (en) | 2006-11-22 | 2011-08-30 | Lockheed Martin Corporation | Over-wing traveling-wave axial flow plasma accelerator |
US7870720B2 (en) * | 2006-11-29 | 2011-01-18 | Lockheed Martin Corporation | Inlet electromagnetic flow control |
DE102006059264A1 (en) * | 2006-12-15 | 2008-06-19 | Thales Electron Devices Gmbh | Plasma accelerator arrangement |
EP2118003A4 (en) * | 2007-03-01 | 2017-12-27 | Plasmatrix Materials AB | Method, material and apparatus for enhancing dynamic stiffness |
FR2919755B1 (en) * | 2007-08-02 | 2017-05-05 | Centre Nat De La Rech Scient (C N R S ) | HALL EFFECT ELECTRON EJECTION DEVICE |
US8407979B1 (en) | 2007-10-29 | 2013-04-02 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Magnetically-conformed, variable area discharge chamber for hall thruster, and method |
JP5037630B2 (en) * | 2007-12-18 | 2012-10-03 | キヤノンアネルバ株式会社 | Plasma processing equipment |
US8508134B2 (en) * | 2010-07-29 | 2013-08-13 | Evgeny Vitalievich Klyuev | Hall-current ion source with improved ion beam energy distribution |
RU2542354C1 (en) * | 2013-10-01 | 2015-02-20 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Московский авиационный институт (национальный исследовательский университет)" | Eroding pulse plasma accelerator |
JP6318447B2 (en) * | 2014-05-23 | 2018-05-09 | 三菱重工業株式会社 | Plasma acceleration apparatus and plasma acceleration method |
CN104290926B (en) * | 2014-09-05 | 2016-05-11 | 兰州空间技术物理研究所 | The high temperature resistant magnet exciting coil of a kind of electric thruster |
DE202015000302U1 (en) | 2015-01-14 | 2015-05-26 | Alexander Rubinraut | Cryogenic electric hall nozzle drive |
FR3032325A1 (en) * | 2015-01-30 | 2016-08-05 | Snecma | HALL EFFECTOR AND SPACE ENGINE COMPRISING SUCH A PROPELLER |
EP3560298A4 (en) * | 2016-12-21 | 2020-08-12 | Phase Four, Inc. | Plasma production and control device |
US9934929B1 (en) | 2017-02-03 | 2018-04-03 | Colorado State University Research Foundation | Hall current plasma source having a center-mounted or a surface-mounted cathode |
US20190107103A1 (en) | 2017-10-09 | 2019-04-11 | Phase Four, Inc. | Electrothermal radio frequency thruster and components |
CN111648930B (en) * | 2020-05-19 | 2021-06-04 | 上海空间推进研究所 | Optimal configuration method for Hall thruster power supply and distribution module architecture |
CN112696330B (en) * | 2020-12-28 | 2022-09-13 | 上海空间推进研究所 | Magnetic pole structure of Hall thruster |
CN113266542B (en) * | 2021-06-29 | 2022-05-17 | 哈尔滨工业大学 | Hall thruster magnetic circuit heat radiation structure |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3613370A (en) * | 1969-11-26 | 1971-10-19 | Nasa | Ion thruster |
JPS6161345A (en) * | 1984-08-31 | 1986-03-29 | Univ Kyoto | Whole accelerator with magnetron auxiliary discharge |
US4841197A (en) * | 1986-05-28 | 1989-06-20 | Nihon Shinku Gijutsu Kabushiki Kaisha | Double-chamber ion source |
US4862032A (en) * | 1986-10-20 | 1989-08-29 | Kaufman Harold R | End-Hall ion source |
SU1715183A1 (en) * | 1990-04-11 | 1994-04-30 | Опытное конструкторское бюро "Факел" | Plasma accelerator with anode layer |
EP0463408A3 (en) | 1990-06-22 | 1992-07-08 | Hauzer Techno Coating Europe Bv | Plasma accelerator with closed electron drift |
US5359258A (en) * | 1991-11-04 | 1994-10-25 | Fakel Enterprise | Plasma accelerator with closed electron drift |
EP0541309B1 (en) * | 1991-11-04 | 1996-01-17 | Fakel Enterprise | Plasma accelerator with closed electron drift |
FR2693770B1 (en) * | 1992-07-15 | 1994-10-14 | Europ Propulsion | Closed electron drift plasma engine. |
RU2022167C1 (en) * | 1992-10-07 | 1994-10-30 | Опытное конструкторское бюро "Факел" | Plasma engine with closed drift of electrons |
RU2030134C1 (en) * | 1992-11-02 | 1995-02-27 | Опытное конструкторское бюро "Факел" | Plasma acceleration with closed electron drift |
RU2045134C1 (en) * | 1993-03-15 | 1995-09-27 | Игорь Борисович Сорокин | Plasma accelerator with closed drift of electrons |
EP0662195B1 (en) * | 1993-06-21 | 1996-08-28 | Societe Europeenne De Propulsion | Reduced length plasma engine with closed electron deviation |
-
1996
- 1996-04-01 RU RU9696105557A patent/RU2092983C1/en active
- 1996-12-03 EP EP96308750A patent/EP0800197B1/en not_active Expired - Lifetime
- 1996-12-03 DE DE69634872T patent/DE69634872T2/en not_active Expired - Lifetime
- 1996-12-03 AT AT96308748T patent/ATE298460T1/en not_active IP Right Cessation
- 1996-12-03 AT AT96308750T patent/ATE298461T1/en not_active IP Right Cessation
- 1996-12-03 DE DE69634871T patent/DE69634871T2/en not_active Expired - Lifetime
- 1996-12-03 EP EP96308748A patent/EP0800196B1/en not_active Expired - Lifetime
- 1996-12-09 US US08/761,948 patent/US5847493A/en not_active Expired - Lifetime
- 1996-12-09 US US08/760,952 patent/US5751113A/en not_active Expired - Lifetime
-
1997
- 1997-03-31 WO PCT/RU1997/000092 patent/WO1997037519A1/en active Search and Examination
Also Published As
Publication number | Publication date |
---|---|
EP0800196B1 (en) | 2005-06-22 |
DE69634872T2 (en) | 2005-11-24 |
US5751113A (en) | 1998-05-12 |
RU2092983C1 (en) | 1997-10-10 |
ATE298461T1 (en) | 2005-07-15 |
DE69634871D1 (en) | 2005-07-28 |
EP0800197A1 (en) | 1997-10-08 |
DE69634872D1 (en) | 2005-07-28 |
DE69634871T2 (en) | 2005-11-24 |
WO1997037519A1 (en) | 1997-10-09 |
EP0800197B1 (en) | 2005-06-22 |
US5847493A (en) | 1998-12-08 |
EP0800196A1 (en) | 1997-10-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |